Busca avançada
Ano de início
Entree


Searching for orbits around the triple system 45 Eugenia

Texto completo
Autor(es):
Mescolotti, B. Y. P. M. ; Prado, A. F. B. A. ; Chiaradia, A. P. M. ; Gomes, V. M. ; IOP
Número total de Autores: 5
Tipo de documento: Artigo Científico
Fonte: WAKE CONFERENCE 2021; v. 911, p. 6-pg., 2017-01-01.
Resumo

Asteroids are small bodies that raises high interest, because they have unknown characteristics. The present research aims to study orbits for a spacecraft around the triple asteroid 45 Eugenia. The quality of the observations made by the spacecraft depends on the distance the spacecraft remains from the bodies of the system. It is used a semi-analytical model that is simple but able to represent the main characteristics of that system. This model is called "Precessing Inclined Bi-Elliptical Problem" (PIBEP). A reference system centered on the main body (Eugenia) and with the reference plane assumed to be in the orbital plane of the second more massive body, here called Petit-Prince, is used. The secondary bodies are assumed to be in elliptical orbits. In addition, it is assumed that the orbits of the smaller bodies are precessing due to the presence of the flattening of the main body (J(2)). This work analyzes orbits for the spacecraft with passages near Petit-Prince and Princesses, which are the two smaller bodies of the triple system. (AU)

Processo FAPESP: 11/13101-4 - Estudo de manobras orbitais para escape de colisão de um veículo espacial com grupos de partículas
Beneficiário:Vivian Martins Gomes
Modalidade de apoio: Auxílio à Pesquisa - Jovens Pesquisadores
Processo FAPESP: 11/08171-3 - Dinâmica orbital de pequenos corpos
Beneficiário:Othon Cabo Winter
Modalidade de apoio: Auxílio à Pesquisa - Temático
Processo FAPESP: 16/14665-2 - Astrodinâmica Aplicada a Veículos Espaciais
Beneficiário:Antônio Fernando Bertachini de Almeida Prado
Modalidade de apoio: Auxílio à Pesquisa - Regular